Application for Spacecraft of the 90's Using MicroDACS Technology

Application for Spacecraft of the 90's Using MicroDACS Technology

International Telemetering Conference Proceedings / October 17-20, 1988 / Riviera Hotel, Las Vegas, Nevada === Recent developments in electronics have made possible the miniaturization of many of the subsystem components associated with a typical spacecraft data acquisition and control system. This...

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Main Author: Horn, Paul
Other Authors: SCI Technology Inc.
Language:en_US
Published: International Foundation for Telemetering 1988
Online Access:http://hdl.handle.net/10150/615031
http://arizona.openrepository.com/arizona/handle/10150/615031
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spelling ndltd-arizona.edu-oai-arizona.openrepository.com-10150-6150312016-07-01T03:01:06Z Application for Spacecraft of the 90's Using MicroDACS Technology Horn, Paul SCI Technology Inc. International Telemetering Conference Proceedings / October 17-20, 1988 / Riviera Hotel, Las Vegas, Nevada Recent developments in electronics have made possible the miniaturization of many of the subsystem components associated with a typical spacecraft data acquisition and control system. This paper describes a low power consumption, fault tolerant, high performance data acquisition and control system design utilizing third generation hardware. The system includes built in test autonomy, redundancy management and fault tolerant communication busses, and supports multiprocessing with up to five 35 Million instructions per second (Mips) processors. 1988-10 text Proceedings 0884-5123 0074-9079 http://hdl.handle.net/10150/615031 http://arizona.openrepository.com/arizona/handle/10150/615031 International Telemetering Conference Proceedings en_US http://www.telemetry.org/ Copyright © International Foundation for Telemetering International Foundation for Telemetering
collection NDLTD
language en_US
sources NDLTD
description International Telemetering Conference Proceedings / October 17-20, 1988 / Riviera Hotel, Las Vegas, Nevada === Recent developments in electronics have made possible the miniaturization of many of the subsystem components associated with a typical spacecraft data acquisition and control system. This paper describes a low power consumption, fault tolerant, high performance data acquisition and control system design utilizing third generation hardware. The system includes built in test autonomy, redundancy management and fault tolerant communication busses, and supports multiprocessing with up to five 35 Million instructions per second (Mips) processors.
author2 SCI Technology Inc.
author_facet SCI Technology Inc.
Horn, Paul
author Horn, Paul
spellingShingle Horn, Paul
Application for Spacecraft of the 90's Using MicroDACS Technology
author_sort Horn, Paul
title Application for Spacecraft of the 90's Using MicroDACS Technology
title_short Application for Spacecraft of the 90's Using MicroDACS Technology
title_full Application for Spacecraft of the 90's Using MicroDACS Technology
title_fullStr Application for Spacecraft of the 90's Using MicroDACS Technology
title_full_unstemmed Application for Spacecraft of the 90's Using MicroDACS Technology
title_sort application for spacecraft of the 90's using microdacs technology
publisher International Foundation for Telemetering
publishDate 1988
url http://hdl.handle.net/10150/615031
http://arizona.openrepository.com/arizona/handle/10150/615031
work_keys_str_mv AT hornpaul applicationforspacecraftofthe90susingmicrodacstechnology
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